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                 384    Mechanical Engineering Design
                  Figure 7–13               y                 Unit load
                                                      a              b j
                                                       j
                  The influence coefficient δ ij
                                               x
                  is the deflection at i due to a  i
                  unit load at j.                                              x
                                                          l

                                          Computer assistance is often used to lessen the difficulty in finding transverse deflections
                                          of a stepped shaft. Rayleigh’s equation overestimates the critical speed.
                                              To counter the increasing complexity of detail, we adopt a useful viewpoint.
                                          Inasmuch as the shaft is an elastic body, we can use influence coefficients. An influence
                                          coefficient is the transverse deflection at location i on a shaft due to a unit load at loca-
                                          tion  j on the shaft. From Table A–9–6 we obtain, for a simply supported beam with a
                                          single unit load as shown in Fig. 7–13,

                                                              ⎧
                                                                b j x i
                                                                          2
                                                                      2
                                                              ⎪      l − b − x 2
                                                              ⎪           j   i          x i ≤ a i
                                                                6EIl
                                                              ⎪
                                                              ⎨
                                                         δ ij =                                            (7–24)
                                                              ⎪ a j (l − x i )    2  2
                                                              ⎪          2lx i − a − x   x i > a i
                                                              ⎪                j    i
                                                              ⎩   6EIl
                                          For three loads the influence coefficients may be displayed as
                                                          j
                                           i      1       2      3
                                           1      δ 11   δ 12    δ 13
                                           2      δ 21   δ 22    δ 23
                                           3      δ 31   δ 32    δ 33


                                                                   6
                                          Maxwell’s reciprocity theorem states that there is a symmetry about the main diago-
                                          nal, composed of δ 11 , δ 22 , and δ 33 , of the form δ ij = δ ji . This relation reduces the work
                                          of finding the influence coefficients. From the influence coefficients above, one can find
                                          the deflections y 1 , y 2 , and y 3 of Eq. (7–23) as follows:

                                                                 y 1 = F 1 δ 11 + F 2 δ 12 + F 3 δ 13
                                                                                                           (7–25)
                                                                 y 2 = F 1 δ 21 + F 2 δ 22 + F 3 δ 23
                                                                 y 3 = F 1 δ 31 + F 2 δ 32 + F 3 δ 33
                                                                                                         2
                                          The forces  F i can arise from weight attached w i or centrifugal forces m i ω y i . The
                                          equation set (7–25) written with inertial forces can be displayed as
                                                                   2          2          2
                                                           y 1 = m 1 ω y 1 δ 11 + m 2 ω y 2 δ 12 + m 3 ω y 3 δ 13
                                                                   2          2          2
                                                           y 2 = m 1 ω y 1 δ 21 + m 2 ω y 2 δ 22 + m 3 ω y 3 δ 23
                                                                   2          2          2
                                                           y 3 = m 1 ω y 1 δ 31 + m 2 ω y 2 δ 32 + m 3 ω y 3 δ 33


                                          6 Thomson, op. cit., p. 167.
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